Snubber-vibration damper system for a bearingless main rotor
AssigneeSikorsky Aircraft Corporation
InventorsDavid N. Schmaling, Robert Milne
Life of this patent
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AssigneeSikorsky Aircraft Corporation
InventorsDavid N. Schmaling, Robert Milne
Estimating the term…
A flexbeam rotor system includes an intermediate tube and a torque tube that envelopes a flexbeam in spaced relation thereto. The torque tube is connected to the flexbeam at its radially outer end and articulately connected to the intermediate tube through a snubber-vibration damper system. The torque tube is connected with an aerodynamic rotor blade member. The snubber vibration damper system includes a snubber bearing and an independent lead/lag bearing. The snubber bearing is located between the flexbeam and the intermediate tube along a pitch change axis. A lead/lag bearing is mounted between the intermediate tube and the torque tube on both the leading and trailing portion of blade assembly. Pitch/lag coupling complications are minimized as lead/lag motion takes place between the torque tube and the intermediate tube. As lead/lag motion is accommodated in the independent lead/lag bearing, the snubber bearing is of a greatly reduced height in relation to conventional design. The overall size of the torque tube is accordingly reduced which advantageously reduces system weight and drag.
A snubber-vibration damper system for a rotor blade assembly comprising:
A snubber-vibration damper system for a rotor blade assembly comprising:
Dependencies are inferred from the claim text.